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Detection device of space electrons

A detection device and electronic technology, applied in measurement devices, radiation measurement, X/γ/cosmic radiation measurement, etc., can solve problems such as miniaturization, low power consumption, large size and quality of detectors that are difficult to meet , to achieve the effect of low power consumption and high resolution

Active Publication Date: 2012-06-20
NO 510 INST THE FIFTH RES INST OFCHINA AEROSPAE SCI & TECH
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

The magnetic deflection method requires high voltage and permanent magnets. Both the electrostatic analyzer method and the time-of-flight method require high voltage to form a strong electric field to accelerate electrons. Although these three detection methods can detect electrons, they need to introduce magnets into the detector. Or high-voltage electric field, resulting in a large volume and mass of the detector, it is difficult to meet the requirements of miniaturization and low power consumption of the detector in the space exploration activities

Method used

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  • Detection device of space electrons
  • Detection device of space electrons
  • Detection device of space electrons

Examples

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Embodiment

[0040] A detection method for space electrons, the method includes a detector and a signal processing circuit.

[0041] The detector is composed of a probe, a heavy metal shell 1-19 and a metal base 1-15, wherein the probe is mainly composed of a light shield 1-3, a detection unit D11-4, a detection unit D21-8, a scintillator frame 1-6, Composed of a photomultiplier tube 1-10 and an analog processing circuit board 1-17, wherein the scintillator frame 1-6 is wrapped around the detection unit D11-4 and the detection unit D21-8;

[0042] The light blocking sheet 1-3 is aluminum foil with a thickness of 60 μm; the detection unit D11-4 is a double-sided silicon microstrip detector with a thickness of 200 μm; the detection unit D21-8 is an ion-implanted PIN silicon detector with a thickness of 2600 μm. 1.92cm, the half angle 1-1 of the formed telescope is 30°; the thickness of the photomultiplier tube 1-10 is 4.45cm; the detection unit D1 and the detection unit D2 are used to detect...

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Abstract

The invention discloses a detection device of space electrons, which belongs to the field of detection of space charged particles. Equipment used by the device comprises a detector and a signal processing circuit, wherein the detector comprises a probe, a heavy metal housing and a metal base; and the probe mainly comprises a light-blocking sheet, a detection unit D1, a detection unit D2, a scintillator framework, a photomultiplier tube and an analog processing circuit board. According to a method disclosed by the invention, a space 0.1-1MeV electron energy spectrum can be detected; and the detector designed by utilizing the method has the characteristics of miniaturization, low power consumption, high resolution and high efficiency, and is convenient to be carried on a spacecraft for detection.

Description

technical field [0001] The invention relates to a detection device for space electrons, in particular to a detection device for 0.1-1 MeV electrons, and belongs to the field of detection of space charged particles. Background technique [0002] The traditional methods for detecting low-energy electrons in space are magnetic deflection method, electrostatic analyzer method and time-of-flight method. The magnetic deflection method requires high voltage and permanent magnets. Both the electrostatic analyzer method and the time-of-flight method require high voltage to form a strong electric field to accelerate electrons. Although these three detection methods can detect electrons, they need to introduce magnets into the detector. Or a high-voltage electric field, resulting in a large volume and mass of the detector, which is difficult to meet the requirements of miniaturization and low power consumption of the detector in the current aerospace exploration activities. Contents ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01T1/00
Inventor 把得东薛玉雄杨生胜安恒石红
Owner NO 510 INST THE FIFTH RES INST OFCHINA AEROSPAE SCI & TECH
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